Numerical Procedure for the Estimation of the Aeroelastic Divergence Limit of a Composite Aircraft Wing using Higher Order Aerodynamics

Summary

This is a publication. If there is no link to the publication on this page, you can try the pre-formated search via the search engines listed on this page.

Authors: Kafkas Angelos; Lampeas George

Journal number: 1

Journal publisher: 9th EASN International Conference

Published year: 2019

DOI identifier: 10.5281/zenodo.4710700